An investigation of oscillations in an adaptive aircraft control system under large input commands.
Approved for public release, distribution unlimited === An adaptive control scheme for aircraft was studied to find the cause of limit cycles which occurred under large input commands and to find a method for eliminating the oscillations. The complexity of the system equations dictated that all anal...
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| Language: | en_US |
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Monterey, California. Naval Postgraduate School
2014
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| Online Access: | http://hdl.handle.net/10945/40133 |